NSN 5990-00-341-3194

Part Details | CONTROL TRANSFORMER SYNCHRO

5990-00-341-3194 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the rotor is dependent upon both the position of the rotor and the electrical input to the stator from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, or variable transformers.

Alternate Parts: TD08382, 610547000, 610547-000, 26V11CT4D, M20708701D, M20708/7-01D, M207087001, M20708/7-001, M207087C001, M20708-7C001, MILS207087C001, MILS20708-7C001, MILS20708726V11CT4, MILS20708-7-26V11CT4, MILS207087, MIL-S-20708/7, 96364, 9636-4, 207087C001, 20708/7C-001, 26V11CT4B, 5990-00-341-3194, 00-341-3194, 5990003413194, 003413194

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 06, 197400-341-319415289 ( SYNCHRO, CONTROL TRANSFORMER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND B

Cross Reference | NSN 5990-00-341-3194
Part Number Cage Code Manufacturer
TD0838213672COMMANDER NAWC-WD
610547-00056232LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN
26V11CT4D81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/7-01D81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/7-00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708-7C00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MILS20708-7C00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MILS20708-7-26V11CT481349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/781349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
9636-403956NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS
20708/7C-00152013SMITHS AEROSPACE INCELECTRONIC SYSTEMS - MALVERN DIV
26V11CT4B10651VERNITRON CORP
Technical Data | NSN 5990-00-341-3194
Characteristic Specifications
STATOR INPUT VOLTAGE RATING IN VOLTS11.8 NOMINAL
STATOR INPUT CURRENT RATING86.0 MILLIAMPERES MAXIMUM
STATOR INPUT ELECTRICAL POWER RATING150.0 WATTS NOMINAL
FREQUENCY IN HERTZ396.0 MINIMUM AND 404.0 MAXIMUM
ZSO IMPEDANCE MAGNITUDE IN OHMS118.00 MINIMUM AND 150.00 MAXIMUM
ZSO IMPEDANCE ANGLE IN DEG78.00 MINIMUM AND 84.00 MAXIMUM
ZRS IMPEDANCE MAGNITUDE IN OHMS130.00 MINIMUM AND 170.00 MAXIMUM
ZRS IMPEDANCE ANGLE IN DEG23.00 MINIMUM AND 35.00 MAXIMUM
PHASE SHIFT ANGLE IN DEG3.000 INPUT TO OUTPUT MINIMUM AND 6.000 INPUT TO OUTPUT MAXIMUM
MAXIMUM TEMP RISE10.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT15.00 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT18.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM7.0/P7.0
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS0.07 INCH-OUNCES MAXIMUM
BODY STYLE STANDARD ROUND B
SHOULDER DIAMETER1.0000 INCHES MAXIMUM
PILOT DIAMETER0.6250 INCHES MAXIMUM
OVERALL LENGTH2.3560 INCHES NOMINAL
FLANGE DIAMETER1.0620 INCHES MAXIMUM
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0620 INCHES NOMINAL
SHOULDER LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.7320 INCHES MAXIMUM
SECURING HOLE QUANTITY4
MOUNTING FACILITY SCREW THREAD SERIES DESIGNATOR UNC
MOUNTING FACILITY NOMINAL SCREW THREAD DIAMETER0.112 INCHES
TERMINAL TYPE AND QUANTITY5 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING
TEST DATA DOCUMENT81349-MIL-S-20708 SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTING GENERAL TYPE DATA ON CERTAIN ENVIRONMENTAL AND PERFORMANCE REQUIREMENTS AND TEST CONDITIONS THAT ARE SHOWN AS "TYPICAL", "AVERAGE", "NOMINAL", ETC.).